GNC Orbit Controls Engineer

Xona Space Systems, Inc

$90K — $130K *
Aerospace & Defense
Less than 5 years of experience
Job Overview by Ladders

Qualifications

  • Familiar with orbital mechanics and simulation; exposure to onboard propagators with perturbation models.
  • GNC software experience in C++ and MATLAB for analysis and test-vector generation.
  • Supported real maneuvers; reconciled planning versus actual results.
  • Comfortable at the ADCS and propulsion interface for burn pointing and momentum management.

Responsibilities

  • Develop open-loop and closed-loop controllers for various altitude management tasks.
  • Implement and maintain onboard orbit propagators and validate their numerical accuracy.
  • Build orbit determination pipelines using Extended Kalman Filters with GNSS data.
  • Design and optimize trajectories, considering various operational constraints.
  • Coordinate burn strategies with ADCS for effective momentum management.
  • Maintain MATLAB and C++ simulators and conduct testing, including Monte Carlo campaigns.
Full Job Description
We9re looking for a GNC Orbit Controls Engineer to design and implement the algorithms and onboard software that handle orbit determination, guidance, maneuver execution, and post-maneuver analysis to deliver safe, efficient, and highly automated station-keeping and disposal. We9re building the software that keeps our spacecraft exactly where they need to be. What You9ll Do
  • Develop open-loop and closed-loop controllers for altitude management, station-keeping, and end-of-life disposal
  • Implement and maintain onboard orbit propagators, select and validate integrators, and ensure numerical consistency with ground truth
  • Build orbit determination pipelines using EKF with GNSS
  • Design burns and long-arc trajectories, and optimize delta V and timelines under comm visibility, power and thermal, and operations constraints
  • Coordinate burn pointing and wheel momentum strategy with ADCS
  • Maintain numerically consistent MATLAB and C++ simulators, create Monte Carlo campaigns, run SIL and HIL tests, and perform post-maneuver reconstruction
Required Qualifications
  • You are familiar with orbital mechanics and simulation and have had exposure with onboard propagators with perturbation models and integrators on flight targets
  • You have GNC software experience in C++ and MATLAB for analysis, modeling, and test-vector generation
  • You have supported real maneuvers and can reconcile plan versus truth with post-burn estimation
  • You are comfortable at the ADCS and propulsion interface for burn pointing and momentum management
Desired Qualifications
  • B.S. or M.S. in Aerospace Engineering, Control Systems, Applied Physics, or a related field
  • Familiar with electric propulsion including thrust modeling and calibration, long-burn guidance, duty-cycle planning, and thermal constraints
  • Experience with orbit propagation algorithms
  • Trajectory design and optimization expertise
  • Familiarity with CCSDS ephemeris and attitude formats
For U.S. Roles: To comply with U.S. Government space technology export regulations, applicant must be a U.S. citizen, lawful permanent resident of the United States (i.e. Green Card holder), or other protected individual as defined by 8 U.S.C. 1324b(a)(3). For U.K. Roles: To comply with U.K. regulations, this role requires Baseline Personnel Security Standard (BPSS) checks, and successful candidates must be eligible to obtain UK Security Clearance (SC).

For Canada Roles: Successful candidates must obtain and hold a security clearance at the reliability status level, and pass security assessment for the Canadian Controlled Goods Program (CGP) and ITAR.

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